Aircraft Loads & Dynamics Engineer - 078QE

Quartus Engineering•Herndon, VA

7d•$142,245 - $235,409•Hybrid

About The Position

Quartus Engineering Incorporated is seeking a highly skilled and experienced Aircraft Loads and Dynamics Engineer to join their team. As a Lead Engineer, this role is critical in evaluating, analyzing, and optimizing the loads and dynamic behavior of aircraft structures and systems. The position requires an advanced understanding of structural loads, aeroelasticity, dynamic response, and certification processes for both fixed-wing and/or rotary-wing aircraft. The candidate should have at least 10 years of industry experience in the aerospace sector, with demonstrated expertise in loads and dynamics analysis and compliance with applicable regulations (e.g., FAR/CS Part 23, 25, 27, or 29). Additionally, experience in sustained engine imbalance analysis and requirements development is a plus.

Requirements

BS and/or MS in Mechanical, Aerospace, Structural, or similar Engineering field
10+ years of experience in aircraft/rotorcraft static loads and criteria
Experience with static and dynamic load derivation for aircraft
Experience developing aeroelastic analysis models
Experience or expertise in MSC NASTRAN, ZAERO, or similar tool is required
Experience or expertise in coding with MATLAB and/or Python
Familiarity with Patran, FEMAP, RCAS, Adams, or comparable tools
Experience with ground vibration and/or static load tests
Experience with Special Class Airworthiness (Part 21)
Must be a US Person (US Citizen or US Permanent Resident)

Nice To Haves

Knowledge and experience with CFD analysis
Experience working with Structures FAA DERs a plus
Knowledge or experience with Aeroservoelastic analyses
Experience in sustained engine imbalance analysis and requirements development is a plus.

Responsibilities

Perform static and dynamic loads analysis for various flight and ground conditions, including gust, turbulence, landing, taxiing, takeoff, and emergency maneuvers.
Develop load cases in compliance with certification requirements and design criteria.
Support the development of aerodynamic databases and load envelopes in coordination with the aerodynamics group.
Conduct aeroelastic analyses, including flutter, divergence, and control reversal studies, to ensure structural stability (FAR 25.629).
Mitigate risks related to structural resonance, fatigue, and dynamic instabilities.
Perform analysis to evaluate the effects of sustained engine imbalance (e.g., rotor unbalance or blade loss) on aircraft structural loads and dynamic response, ensuring compliance with regulatory standards (e.g., CFR 25.901(c), 25.903(c), AC 25-24).
Prepare technical reports, substantiation documents, and compliance data packages for regulatory authorities (e.g., FAA, EASA).
Ensure compliance with applicable airworthiness standards (e.g., CFR/CS Part 23, 25, 27, 29).
Collaborate with regulatory agencies and certification specialists as needed.
Provide technical guidance and mentorship to junior engineers and team members.
Work directly with Quartus’s business development/sales organization to expand and diversify our air vehicle customer base.